Patent US-1914-1166879
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Projectile can follow a flattened or curved trajectory as desired ; braking device
- Tech class CPC F42B10/14: Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
- Inventor location: 28 Avenue de Wagram, Paris, France
- Witnesses as shown on the final text page: Louis Fautrat and Hanson C. Coxe
Sources
- Patent 1166879 document and bibliographic info on espacenet
- Patent 1166879 at google patents
Year filed | 1914 |
---|---|
Year granted | 1916 |
Office | US |
Patent number | 1166879 |
Inventors | Louis Alard |
Inventor country | FR |
Applicant person | Louis Alard |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | Yes |
Original title | Apparatus for modifying the trajectory of a projectile |
English title | Apparatus for modifying the trajectory of a projectile |
Tech fields | projectile, control |
Filing date | 1914/01/27 |
Full specification filed date | |
Application number | |
Grant date | 1916/01/04 |
Granted? | Yes |
Publication date | |
Supplementary to patent | Patent FR-1913-466195 |
Related to aircraft? | 0.5 |
Serial number | 814639 |
Patent agent | A-something S U-something |
Assigned to | |
National tech categories | USPC 244/3.29, USPC 102/400 |
IPCs | IPC F42B10/14, IPC F42B 10/00 |
CPCs | CPC F42B10/14 |
Family year | 1914 |
First filing? | Yes |
Cites these patents | |
Citations from after 1930 | 20 |
Application ID | |
INPADOC family ID | |
Number of text pages | 5 |
Number of diagram pages | 10 |
Number of figures | 29 |
Number of claims | 6 |